US3901988A - Inflatable trunk for air cushion supported vehicles - Google Patents
Inflatable trunk for air cushion supported vehicles Download PDFInfo
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- US3901988A US3901988A US421335A US42133573A US3901988A US 3901988 A US3901988 A US 3901988A US 421335 A US421335 A US 421335A US 42133573 A US42133573 A US 42133573A US 3901988 A US3901988 A US 3901988A
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- Prior art keywords
- opening
- pair
- trunk
- tapes
- sheet
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- 238000004519 manufacturing process Methods 0.000 claims abstract description 34
- 239000004744 fabric Substances 0.000 claims abstract description 30
- 239000011159 matrix material Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims description 26
- 239000013013 elastic material Substances 0.000 claims description 4
- 230000000694 effects Effects 0.000 abstract description 5
- 239000000835 fiber Substances 0.000 abstract description 3
- 238000010276 construction Methods 0.000 description 11
- 238000000034 method Methods 0.000 description 5
- 239000004677 Nylon Substances 0.000 description 4
- 229920001778 nylon Polymers 0.000 description 4
- 238000011068 loading method Methods 0.000 description 3
- 238000003491 array Methods 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 239000012783 reinforcing fiber Substances 0.000 description 2
- 210000001015 abdomen Anatomy 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 244000309464 bull Species 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D22/00—Producing hollow articles
- B29D22/02—Inflatable articles
- B29D22/023—Air springs; Air bellows
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
- B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F3/00—Devices, e.g. jacks, adapted for uninterrupted lifting of loads
- B66F3/24—Devices, e.g. jacks, adapted for uninterrupted lifting of loads fluid-pressure operated
- B66F3/25—Constructional features
- B66F3/35—Inflatable flexible elements, e.g. bellows
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1334—Nonself-supporting tubular film or bag [e.g., pouch, envelope, packet, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
Definitions
- the fabric of the invention is a laminate of tensile fibers in an elastomeric matrix, which is elastic (to different degrees and within different limitations in different directions) and is patterned to incorporate within various areas thereof specifically dimensioned small area slots or e1- liptically shaped openings therethrough, which upon inflation of the trunk and consequent girthwise extension of the fabrication open up into relatively large area, substantially circularly shaped ports, for delivery of air through the trunk against a reaction surface.
- This invention relates to air cushion" supported machines, such as airplanes of the type disclosed for example in US. Reissue Pat. No. 26,8l2. or ground effect machines such as disclosed for example in US. Pat. No. 3,365 .017; which machines employ inflated trunk type arrangements for confining the machine lift air cushion. More specifically, the invention relates to a trunk construction fabric for such purposes whereby the air exit apertures therethrough (as shown for example at 24 in U.S. Pat. No. 3.69(),40l) are provided for by means of an improved laminate layup system which results in an improved fabric construction for the intended usage.
- the fabrication comprises a lamination of parallel arrays of longitudinally coiled or undulant or otherwise elastically extendible (within limits) high tensile strength strands extending in the girthwise directions of the wall structure, in combination with cross-laid rigid or low-elastic high tensile strength strands disposed to extend in the lengthwise directions of the trunk structure; all embodied within or in layered association with an air-sealing elastomeric matrix or sheet(s).
- the trunk cell structure is readily adaptable to girthwise expansion-contraction deformation (but only within prescribed limits) to provide improved elastic expansion control procedures throughout various sections of the structure so as to regulate the inflated shape of the structure. while also being operable to resist deformations of the inflated shape of the fore-andaft directions of the structure incidental to taxiing. takeoff. and landing maneuvers of the aircraft.
- a stockpiece of differentially flexible/elastic sheet material may be fabricated and tailored" to the prescribed trunk system planform as well as to any typically encountered three-dimensionally curviformed fuselage to which it is to be attached; so that when the trunk struc ture so produced is inflated it will assume the desired balloonlike configuration without inherent fabric stress concentrations at localized areas thereof.
- the structure When deflated. the structure will by nature retract and compactly hug the hull or fuselage or frame of the attended vehicle, as the case may be.
- the system When inflated. the system features improved resistance to planform distortion, such as would otherwise occur and adversely affect the vehicle support air cushion effect" operation.
- the present invention provides for an improved construction ambient to the air exit ports through the fabric; and in consequence. integrity of the prescribed air cushion space planform shape and dimensions is preserved. and the trunk structure is better protected against wear and tear damage.
- the stocksheet fabrication preferably comprises transversely disposed multiple layers of tapes embodying the strands referred to hereinabove within a matrix as aforesaid.
- the laminate layup design is such that the reinforcing fibers are routed around the initially formed openings through the fabrication during the laminate layout in such manner that no reinforcing fibers are interrupted and so that minimum stress concentrations develop under elastic elongation conditions.
- the perimeters of the ports are structurally reinforced. whereby the ultimate material strength of the fiber/matrix is not reduced and the trunk is of improved resis tance to wear/tear damage.
- the fabrication provides exit ports which are of substantially constant areas throughout the normal operating range of fabric elongation.
- FIG. I is a fragmentary plan view of an airplane such as may advantageously employ an air cushion type undercarriage utilizing an elastic trunk fabric construction of the present invention
- FIG. 2 is a front elevational view thereof
- FIG. 3 is a side elevational view thereof
- FIG. 4 is an enlarged scale fragmentary sectional view of the undercarriage trunk construction. taken as suggested by line 4-4 of FIG. 3;
- FIG. 5 illustrates a fragmentary length of elastic thread such as is used in compounding an elastic trunk fabrication in accordance with the invention
- FIG. 6 is a plan view fragmentary illustration of an initial step in fabricating a tape component of the construction
- FIG. 7 is a sectional view through a typical tape construction fabricated as illustrated by FIG. 6;
- FIG. 8 is a fragmentary plan view illustration of a trunk fabric construction of the present invention showing air escape apertures therethrough as initially formed, and when the fabric is in its relaxed condition;
- FIG. 9 is a sectional view taken as suggested by line 99 of FIG. 8;
- FIG. 10 is a view corresponding to FIG. 8 but showing the fabric in an approximately I00 percent elastically elongated condition (in one direction only). and illustrating the circular configurations consequently assumed by the air escape ports;
- FIG. 11 is a graphical representation of test data illustrating the port-area increase rate relative to applied loading on a typical sample of fabric made in accordance with the invention.
- the invention may be embodied in an air cushion confining trunk system comprising the undercarriage of an airplane wherein the fuselage or hull thereof is indicated generally at 10. More specifically. the trunk system is shown to comprise a rectangularly-toroidal-shaped trunk as indicated generally at I2 which is formed of a special fabric sheeting attached to the belly of the airplane fuselagc to provide an air cushion confining space therebelow.
- the aircraft may be supported in friction-free relation above a reaction surface incidental to landings. takeoffs. and taxiing maneuvers.
- the invention is equally applicable to other air cushion defining inflatable trunk shapes and/or arrangements, such as are typically used in connection with ground effect machines, or the like.
- trunk device 12 As explained in the aforesaid referenced patents. means are provided to deliver the air into the interior of the inflatable trunk device to thereby inflate the latter as shown in the drawing herewith. Furthermore. the bottom footprint" surfaces of trunk device 12 are formed with holes or ports as indicated at 32 (FIG. 4)
- the present invention features employment in such trunk devices as aforesaid, of a novel flexible sheet material fabrication, the method and details of construction thereof being illustrated by FIGS. 5-8 herewith.
- the sheet fabrication as indicated at (FIG. 8) will comprise a combination of layered, transversely disposed stretch control" strands of high tensile strength material such as Nylon, or the like, embedded within or otherwise associated with an airtight film or layer; the various stretch control strands being appropriately and selectively oriented so as to accomplish the objects set forth hereinabove.
- the fabric stocksheet 20 may generally comprise a laminate formed of crossed tapes having different elastic elongation characteristics as will be explained more fully hereinafter; the tapes being enclosed within upper and lower layers of rubber or the like and vulcanized together to form an integrated elastic structure, as best shown at FIGS. 8, 9, 10. All of the tapes include tensile strands of Nylon or the like embedded within a matrix of rubber or the like. As explained in US. Pat. No. 3,690,401 it will be appreciated that the straight-line portions of the trunk sheet need be elastic only in the girthwise directions thereof. However, the rounded corner portions of the trunk sheet must be omnidirectionally elastic in order to provide a trunk system which when inflated will balloon out to the configura tion shown in FIGS. l-4 of the drawing herewith, and the patent explains how the fabrication may be designed to provide the desired smoothly contoured form thereof without internal restraint or stress concentrations in the areas of transition from cylindrically to spherically curved forms.
- the tapes running girthwise of the trunk to be constructed from the fabric may comprise parallel arrays of precoiled (or crimped) Nylon strands designated 26, which are preferably preassembled upon core threads 28 of rubber or the like for convenience in handling (FIG. 5).
- the strands 26 are assembled as shown at FIGS. 6, 7, so as to he sandwiched" between layers 3030 of rubber or the like. to provide the girthwise tapes".
- the crosswise disposed tapes extending lengthwise of the trunk to be constructed from the fabric also comprise rubber matrices having straight (or only slightly coiled or crimped) strands of Nylon. depending upon the stretch characteristics prescribed for the lengthwise run" of the trunk construction; the composite being pressed or heat-rolled together and vulcanized or otherwise adhesively integrated to facilitate handling.
- a multilayered sheet fabrication may be laid down upon a flat work table so as to encompass the plan view dimensioned extent of the prerequiste zones of attachment of the undercarriage structure to the airplane fuselage.
- the stocksheet is then cut or tailored to appropriate shape and dimensions. Any variants of dimensionally elastic/rigid requirements for the various parts of any given trunk planform configuration may thus be readily accommodated. so that the trunk system will expand to the desired form when inflated and will hold this form against shape distortions such as would otherwise be induced by drag forces operating thereon incidental to taxiing, takeoff and landing maneuvers of the craft.
- a trunk system of the invention may be readily fabricated and tailored to the configurations of a large variety of bull shapes, so that in any case when the trunk system is deflated it will elastically contract into flat and smoothly fitting, compactly nested, relation against the vehicle hull; thereby maximizing aerodynamic efficiencies for such craft when so equipped.
- the present invention however deals with the problem of providing the air exit apertures through the fabric such as are illustrated at 32 (FIG. I0 of the drawing herewith); and the method of the invention is illustrated at FIGS. 8, 9, I0.
- the layout table 33 upon which the laminate is formulated is provided with upstanding mandrels or the like as indicated at 34; the mandrels being sectionally shaped and dimensioned to complement the desired shapes and dimensions of the air exit apertures through the fabric when the latter is in its relaxed condition.
- a bottom layer of rubber or the like may be placed on the table and the girthwise and lengthwise tapes as herein above described are then laid down in cross-laminating fashion.
- the tapes are routed around the mandrels during the layup process, whereby none of the tapes and/or the included tensile strands are interrupted by the apertures through the fabrication.
- FIG. 8 This routing process is illustrated at FIG. 8 wherein typical girthwise tapes are designated at 4050 inclusive, and typical lengthwise tapes are indicated at 5257 inclusive. It is to be noted that as the tapes are routed around the mandrels 34 they overlap and thus reinforce the walls of the fabrication circumscribing the mandrels, and that none of the tensile strands interiorly of the tapes are cut or otherwise interrupted. Thus, the fabrication will be built up as is also illustrated at FIG. 9 so as to include as many laminations of cross-laid tapes as may be required in any given in; stance to provide the prescribed sheet fabrication.
- top layer of rubber or the like is applied to the upper surface of the assembly and the entire fabrication is then autoclaved under vacuum and heat so as to compress and vulcanize the assembly into a single integrated sheet like fabric. It will be understood that upon removal of the fabrication from the worktable and the mandrels, the desired air exit apertures will have been formed therethrough; their geometries being complementary to the sectional geometries of the mandrels.
- some of the elastic tapes (such as 43, 46, 49 of the Series 40-50 as 40-50 in FIGS. 8, 10) are routed to pass straight through between the aperture areas or mandrels 34 (as the case may be) in the girthwise direction of the fabric.
- the girthwise elastic tapes 4042, 44, 45, 47, 48 and 50 which are aligned generally with the hole areas are locally offset-diverted so as to pass around the hole areas. They are thereupon realigned in parallel offset relation to provide the de sired elastic continuity in the girthwise direction of the fabric.
- the angularly diverted portions of the tapes introduce lateral tension components in the fabric when stressed which would if unopposed, tend to close the holes when the fabric is tensioned.
- the oppositely paired tapes such as tapes 44-42 and 47-45 characteristically cooperate and balance out the tendencies thereof to transversely "squeeze" or close the holes.
- the elongated S pattern type distortion of each tape as it bypasses the hole area operates to apply substantially equal elongation stresses upon each elastic cord of the tape. Accordingly. undesirable stress anomalies are avoided in the tapes per se. In consequence the overlapped tape portions of successive layers of tapes are of substantially uniform material properties throughout the material thickness, whereby the desired ultimate strength is maintained.
- FIG. illustrates how the fabrication reacts to internal inflationary pressures when employed in the construction of an air cushion confining trunk as explained hereinabove.
- the girthwise extending tape sections will relatively readily elastically extend while the lengthwise disposed tape sections resist or permit only limited extension as the case may be according to the stretch prescription for that portion of the fabrication,
- the relatively small elliptically shaped apertures through the fabrication are now extended so as to open up into substantially circular form as illustrated at 32 in FIG. 10.
- the fabrication is such that when the fabric is elastically extended under normal operating conditions such as to a substantially 100 percent elongated condition (in the girthwise direction) the apertures 32 open up into substantially circular configurations.
- This provides for optimum air jet performance, and it will be appreciated that the fabrication may be readily engineered so that when it is inflated the circular ports provide for the desired rate of delivery of air against the reaction surface and into the air cushion cavity under the vehicle.
- the fabrication may be adapted when inflated to operate over a wide range of loadings as illustrated at FIG. 11, the areas of the ports 32 will remain substantially constant. This is due to the fact that the tape layup permits the holes 32 to elongate in the girthwise direction of the fabric (but only to a prescribed degree) while at the same time the transverse dimensions of the holes and of the intermediate portions of the fabric are substantially maintained. This is ofcourse an important feature from the standpoint of performance of the air trunk system and control of the vehicle operation.
- an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured margin ally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space
- said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising:
- each tape of said first series including a matrix and a plurality of relatively inelastic tension cords embedded in and running lengthwise of such tapes, at least one pair of adjacent tapes of said first series having their adjacent side edges separated for a distance in said one direction by a first spacing in said second direction;
- each tape of said second series including a matrix and a plurality of relatively elastic tension cords embedded in and running lengthwise of such tapes, there being a first separated pair of said tapes of the second series which are parallel and are separated by a second spacing which is greater than said first spacing whereby said first spacing defines the minor axis of an ellipse and said second spacing defines the major axis of such ellipse, said adjacent pair of tapes of the first series being separated in said one direction by at least said second spacing and said separated pair of said tapes of the second series crossing said adjacent pair such that said sheet has an elliptical opening therethrough delineated by said minor and major axes, there being a second pair of tapes of said second series disposed on opposite sides of one of said tapes of the first sepa rated pair, said second pair of tapes criss-crossing each other and said one tape of the first separated pair at one end of said opening, there being a third pair of
- opening means comprise(s) a plurality of elliptically shaped openings arranged with their major axes aligned in row form extending transversely of the relatively elastic direction of said sheet.
- an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured marginally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space
- said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising:
- a sheet-like body of elastic material having at least one elliptical opening therethrough, the minor axis of such opening being aligned in said second direction and the major axis of such opening being aligned in said one direction;
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Abstract
There is disclosed in air cushion type airplane undercarriages, or air cushion vehicle or other ''''surface effect'''' machine air cushion seals of the inflatable trunk type an improved omnidirectionally elastic fabric from which to construct such trunks so as to render the machines supportable by means of air films/cushions relative to reaction surfaces. The fabric of the invention is a laminate of tensile fibers in an elastomeric matrix, which is elastic (to different degrees and within different limitations in different directions) and is patterned to incorporate within various areas thereof specifically dimensioned small area slots or elliptically shaped openings therethrough, which upon inflation of the trunk and consequent girthwise extension of the fabrication open up into relatively large area, substantially circularly shaped ports, for delivery of air through the trunk against a reaction surface.
Description
United States Patent [:91
Coles et al.
1 1 INFLATABLE TRUNK FOR AIR CUSHION SUPPORTED VEHICLES [75] Inventors; Alan V. Coles, Williamsville;
Lawrence H. Kocher, Tonawanda, both of N.Y.
[73] Assignee: Textron, Inc., Providence, R1
[22] Filed: Dec. 3, 1973 [2]] Appl. Now-121,335
[56] References Cited UNITED STATES PATENTS 2,659,957 11/1953 Lilienfcld 161/77 3,455,100 7/1969 Sidles ct 211, 3,485,695 12/1969 Ness 3,642,565 2/1972 Ogata et a1. 161/175 51 Aug. 26, 1975 Earl 161/47 Earl et a1, 244/102 R [57] ABSTRACT There is disclosed in air cushion type airplane undercarriages, or air cushion vehicle or other surface effect" machine air cushion seals of the inflatable trunk type an improved omnidirectionally elastic fabric from which to construct such trunks so as to render the machines supportable by means of air films/cush ions relative to reaction surfaces. The fabric of the invention is a laminate of tensile fibers in an elastomeric matrix, which is elastic (to different degrees and within different limitations in different directions) and is patterned to incorporate within various areas thereof specifically dimensioned small area slots or e1- liptically shaped openings therethrough, which upon inflation of the trunk and consequent girthwise extension of the fabrication open up into relatively large area, substantially circularly shaped ports, for delivery of air through the trunk against a reaction surface.
8 Claims, 11 Drawing Figures PATENTED M182 6 i975 SHEET 2 of 2 LOADING AREA OPERATING RANGE T On O P FIG. 9
INFLATABLE TRUNK FOR AIR CUSHION SUPPORTED VEHICLES BACKGROUND AND GENERAL DESCRIPTION OF THE INVENTION The invention herein described was made in the course of or under a contract with the Department of the Air Force.
This invention relates to air cushion" supported machines, such as airplanes of the type disclosed for example in US. Reissue Pat. No. 26,8l2. or ground effect machines such as disclosed for example in US. Pat. No. 3,365 .017; which machines employ inflated trunk type arrangements for confining the machine lift air cushion. More specifically, the invention relates to a trunk construction fabric for such purposes whereby the air exit apertures therethrough (as shown for example at 24 in U.S. Pat. No. 3.69(),40l) are provided for by means of an improved laminate layup system which results in an improved fabric construction for the intended usage.
The fabrication comprises a lamination of parallel arrays of longitudinally coiled or undulant or otherwise elastically extendible (within limits) high tensile strength strands extending in the girthwise directions of the wall structure, in combination with cross-laid rigid or low-elastic high tensile strength strands disposed to extend in the lengthwise directions of the trunk structure; all embodied within or in layered association with an air-sealing elastomeric matrix or sheet(s). In consequence. the trunk cell structure is readily adaptable to girthwise expansion-contraction deformation (but only within prescribed limits) to provide improved elastic expansion control procedures throughout various sections of the structure so as to regulate the inflated shape of the structure. while also being operable to resist deformations of the inflated shape of the fore-andaft directions of the structure incidental to taxiing. takeoff. and landing maneuvers of the aircraft.
As explained in the aforesaid Patents, with regard to the prescribed planform of a given trunk system, a stockpiece of differentially flexible/elastic sheet material may be fabricated and tailored" to the prescribed trunk system planform as well as to any typically encountered three-dimensionally curviformed fuselage to which it is to be attached; so that when the trunk struc ture so produced is inflated it will assume the desired balloonlike configuration without inherent fabric stress concentrations at localized areas thereof. When deflated. the structure will by nature retract and compactly hug the hull or fuselage or frame of the attended vehicle, as the case may be. When inflated. the system features improved resistance to planform distortion, such as would otherwise occur and adversely affect the vehicle support air cushion effect" operation.
The present invention provides for an improved construction ambient to the air exit ports through the fabric; and in consequence. integrity of the prescribed air cushion space planform shape and dimensions is preserved. and the trunk structure is better protected against wear and tear damage. To this end the stocksheet fabrication preferably comprises transversely disposed multiple layers of tapes embodying the strands referred to hereinabove within a matrix as aforesaid. The laminate layup design is such that the reinforcing fibers are routed around the initially formed openings through the fabrication during the laminate layout in such manner that no reinforcing fibers are interrupted and so that minimum stress concentrations develop under elastic elongation conditions. Incidentally. the perimeters of the ports are structurally reinforced. whereby the ultimate material strength of the fiber/matrix is not reduced and the trunk is of improved resis tance to wear/tear damage. Furthermore. the fabrication provides exit ports which are of substantially constant areas throughout the normal operating range of fabric elongation.
THE DRAWING FIG. I is a fragmentary plan view of an airplane such as may advantageously employ an air cushion type undercarriage utilizing an elastic trunk fabric construction of the present invention;
FIG. 2 is a front elevational view thereof;
FIG. 3 is a side elevational view thereof;
FIG. 4 is an enlarged scale fragmentary sectional view of the undercarriage trunk construction. taken as suggested by line 4-4 of FIG. 3;
FIG. 5 illustrates a fragmentary length of elastic thread such as is used in compounding an elastic trunk fabrication in accordance with the invention;
FIG. 6 is a plan view fragmentary illustration of an initial step in fabricating a tape component of the construction;
FIG. 7 is a sectional view through a typical tape construction fabricated as illustrated by FIG. 6;
FIG. 8 is a fragmentary plan view illustration of a trunk fabric construction of the present invention showing air escape apertures therethrough as initially formed, and when the fabric is in its relaxed condition;
FIG. 9 is a sectional view taken as suggested by line 99 of FIG. 8;
FIG. 10 is a view corresponding to FIG. 8 but showing the fabric in an approximately I00 percent elastically elongated condition (in one direction only). and illustrating the circular configurations consequently assumed by the air escape ports; and
FIG. 11 is a graphical representation of test data illustrating the port-area increase rate relative to applied loading on a typical sample of fabric made in accordance with the invention.
As shown by way of example herein at FIGS. I4. the invention may be embodied in an air cushion confining trunk system comprising the undercarriage of an airplane wherein the fuselage or hull thereof is indicated generally at 10. More specifically. the trunk system is shown to comprise a rectangularly-toroidal-shaped trunk as indicated generally at I2 which is formed of a special fabric sheeting attached to the belly of the airplane fuselagc to provide an air cushion confining space therebelow. Thus. the aircraft may be supported in friction-free relation above a reaction surface incidental to landings. takeoffs. and taxiing maneuvers. It is to be understood however that the invention is equally applicable to other air cushion defining inflatable trunk shapes and/or arrangements, such as are typically used in connection with ground effect machines, or the like.
As explained in the aforesaid referenced patents. means are provided to deliver the air into the interior of the inflatable trunk device to thereby inflate the latter as shown in the drawing herewith. Furthermore. the bottom footprint" surfaces of trunk device 12 are formed with holes or ports as indicated at 32 (FIG. 4)
through which jets of compressed air issue to establish the machine supporting air cushion.
The present invention features employment in such trunk devices as aforesaid, of a novel flexible sheet material fabrication, the method and details of construction thereof being illustrated by FIGS. 5-8 herewith. Basically. the sheet fabrication as indicated at (FIG. 8) will comprise a combination of layered, transversely disposed stretch control" strands of high tensile strength material such as Nylon, or the like, embedded within or otherwise associated with an airtight film or layer; the various stretch control strands being appropriately and selectively oriented so as to accomplish the objects set forth hereinabove.
The fabric stocksheet 20 may generally comprise a laminate formed of crossed tapes having different elastic elongation characteristics as will be explained more fully hereinafter; the tapes being enclosed within upper and lower layers of rubber or the like and vulcanized together to form an integrated elastic structure, as best shown at FIGS. 8, 9, 10. All of the tapes include tensile strands of Nylon or the like embedded within a matrix of rubber or the like. As explained in US. Pat. No. 3,690,401 it will be appreciated that the straight-line portions of the trunk sheet need be elastic only in the girthwise directions thereof. However, the rounded corner portions of the trunk sheet must be omnidirectionally elastic in order to provide a trunk system which when inflated will balloon out to the configura tion shown in FIGS. l-4 of the drawing herewith, and the patent explains how the fabrication may be designed to provide the desired smoothly contoured form thereof without internal restraint or stress concentrations in the areas of transition from cylindrically to spherically curved forms.
Thus, the tapes running girthwise of the trunk to be constructed from the fabric may comprise parallel arrays of precoiled (or crimped) Nylon strands designated 26, which are preferably preassembled upon core threads 28 of rubber or the like for convenience in handling (FIG. 5). The strands 26 are assembled as shown at FIGS. 6, 7, so as to he sandwiched" between layers 3030 of rubber or the like. to provide the girthwise tapes". The crosswise disposed tapes extending lengthwise of the trunk to be constructed from the fabric also comprise rubber matrices having straight (or only slightly coiled or crimped) strands of Nylon. depending upon the stretch characteristics prescribed for the lengthwise run" of the trunk construction; the composite being pressed or heat-rolled together and vulcanized or otherwise adhesively integrated to facilitate handling.
As explained in US. Pat. No. 3,690,401 whenever it is required to provide an appropriately operable inflatable air cushion confining trunk system for such pur poses, a multilayered sheet fabrication may be laid down upon a flat work table so as to encompass the plan view dimensioned extent of the prerequiste zones of attachment of the undercarriage structure to the airplane fuselage. The stocksheet is then cut or tailored to appropriate shape and dimensions. Any variants of dimensionally elastic/rigid requirements for the various parts of any given trunk planform configuration may thus be readily accommodated. so that the trunk system will expand to the desired form when inflated and will hold this form against shape distortions such as would otherwise be induced by drag forces operating thereon incidental to taxiing, takeoff and landing maneuvers of the craft. Furthermore. it will be apparent that a trunk system of the invention may be readily fabricated and tailored to the configurations of a large variety of bull shapes, so that in any case when the trunk system is deflated it will elastically contract into flat and smoothly fitting, compactly nested, relation against the vehicle hull; thereby maximizing aerodynamic efficiencies for such craft when so equipped.
The present invention however deals with the problem of providing the air exit apertures through the fabric such as are illustrated at 32 (FIG. I0 of the drawing herewith); and the method of the invention is illustrated at FIGS. 8, 9, I0. As best shown at FIGS. 8, 9, the layout table 33 upon which the laminate is formulated is provided with upstanding mandrels or the like as indicated at 34; the mandrels being sectionally shaped and dimensioned to complement the desired shapes and dimensions of the air exit apertures through the fabric when the latter is in its relaxed condition. A bottom layer of rubber or the like may be placed on the table and the girthwise and lengthwise tapes as herein above described are then laid down in cross-laminating fashion. It should be particularly noted that in accordance with the present invention the tapes are routed around the mandrels during the layup process, whereby none of the tapes and/or the included tensile strands are interrupted by the apertures through the fabrication.
This routing process is illustrated at FIG. 8 wherein typical girthwise tapes are designated at 4050 inclusive, and typical lengthwise tapes are indicated at 5257 inclusive. It is to be noted that as the tapes are routed around the mandrels 34 they overlap and thus reinforce the walls of the fabrication circumscribing the mandrels, and that none of the tensile strands interiorly of the tapes are cut or otherwise interrupted. Thus, the fabrication will be built up as is also illustrated at FIG. 9 so as to include as many laminations of cross-laid tapes as may be required in any given in; stance to provide the prescribed sheet fabrication. To finalize the fabrication top layer of rubber or the like is applied to the upper surface of the assembly and the entire fabrication is then autoclaved under vacuum and heat so as to compress and vulcanize the assembly into a single integrated sheet like fabric. It will be understood that upon removal of the fabrication from the worktable and the mandrels, the desired air exit apertures will have been formed therethrough; their geometries being complementary to the sectional geometries of the mandrels.
Note that some of the elastic tapes (such as 43, 46, 49 of the Series 40-50 as 40-50 in FIGS. 8, 10) are routed to pass straight through between the aperture areas or mandrels 34 (as the case may be) in the girthwise direction of the fabric. while the girthwise elastic tapes 4042, 44, 45, 47, 48 and 50 which are aligned generally with the hole areas are locally offset-diverted so as to pass around the hole areas. They are thereupon realigned in parallel offset relation to provide the de sired elastic continuity in the girthwise direction of the fabric. Because of the tape routing pattern as shown in the drawing herewith the angularly diverted portions of the tapes (for example, reference may be made to tapes 4247) introduce lateral tension components in the fabric when stressed which would if unopposed, tend to close the holes when the fabric is tensioned. However, note that the oppositely paired tapes, such as tapes 44-42 and 47-45 characteristically cooperate and balance out the tendencies thereof to transversely "squeeze" or close the holes. It should be noted that the elongated S pattern type distortion of each tape as it bypasses the hole area operates to apply substantially equal elongation stresses upon each elastic cord of the tape. Accordingly. undesirable stress anomalies are avoided in the tapes per se. In consequence the overlapped tape portions of successive layers of tapes are of substantially uniform material properties throughout the material thickness, whereby the desired ultimate strength is maintained.
FIG. illustrates how the fabrication reacts to internal inflationary pressures when employed in the construction of an air cushion confining trunk as explained hereinabove. Note that the girthwise extending tape sections will relatively readily elastically extend while the lengthwise disposed tape sections resist or permit only limited extension as the case may be according to the stretch prescription for that portion of the fabrication, As a result thereof the relatively small elliptically shaped apertures through the fabrication are now extended so as to open up into substantially circular form as illustrated at 32 in FIG. 10.
It is to be particularly noted that in the case of the present invention the fabrication is such that when the fabric is elastically extended under normal operating conditions such as to a substantially 100 percent elongated condition (in the girthwise direction) the apertures 32 open up into substantially circular configurations. This provides for optimum air jet performance, and it will be appreciated that the fabrication may be readily engineered so that when it is inflated the circular ports provide for the desired rate of delivery of air against the reaction surface and into the air cushion cavity under the vehicle.
Furthermore, it will be noted that although the fabrication may be adapted when inflated to operate over a wide range of loadings as illustrated at FIG. 11, the areas of the ports 32 will remain substantially constant. This is due to the fact that the tape layup permits the holes 32 to elongate in the girthwise direction of the fabric (but only to a prescribed degree) while at the same time the transverse dimensions of the holes and of the intermediate portions of the fabric are substantially maintained. This is ofcourse an important feature from the standpoint of performance of the air trunk system and control of the vehicle operation.
We claim:
I. In an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured margin ally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space, the improvement wherein said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising:
a first series of tapes associated with said sheet and disposed in sideby-side relation and running in said one direction, each tape of said first series including a matrix and a plurality of relatively inelastic tension cords embedded in and running lengthwise of such tapes, at least one pair of adjacent tapes of said first series having their adjacent side edges separated for a distance in said one direction by a first spacing in said second direction;
a second series of tapes associated with said sheet and running in said second direction, each tape of said second series including a matrix and a plurality of relatively elastic tension cords embedded in and running lengthwise of such tapes, there being a first separated pair of said tapes of the second series which are parallel and are separated by a second spacing which is greater than said first spacing whereby said first spacing defines the minor axis of an ellipse and said second spacing defines the major axis of such ellipse, said adjacent pair of tapes of the first series being separated in said one direction by at least said second spacing and said separated pair of said tapes of the second series crossing said adjacent pair such that said sheet has an elliptical opening therethrough delineated by said minor and major axes, there being a second pair of tapes of said second series disposed on opposite sides of one of said tapes of the first sepa rated pair, said second pair of tapes criss-crossing each other and said one tape of the first separated pair at one end of said opening, there being a third pair of tapes of said second series disposed on opposite sides of the other of said tapes of the first separated pair, said third pair of tapes crisscrossing each other and said other tape of the first separated pair at the other end of said opening whereby when said trunk is uninflated said opening is elliptical whereas when said trunk is inflated said opening will assume a generally circular shape.
2. In an air cushion vehicle as defined in claim 1 wherein said second pair of tapes lie on opposite sides of and in side-by-side relation to said one tape of the first pair except at the crossing region with each other and said one tape, and wherein said third pair of tapes lie on opposite sides of and in side-by-side relation to said other tape of the first pair except at the crossing region with each other and said other tape.
3. In an air cushion vehicle a sheet material fabrication as set forth in claim I, wherein said tension cords are crowded within portions of the fabrication peripherally of said opening means to reinforce the latter.
4. In an air cushion vehicle a sheet material fabrication as set forth in claim 1, wherein all of said tension cords bypass said fabrication opening means and extend thoughout the geometric extent of said fabric sheet without interruption.
5. In an air cushion vehicle a sheet material fabrication as set forth in claim I, wherein said opening means comprise(s) a plurality of elliptically shaped openings arranged with their major axes aligned in row form extending transversely of the relatively elastic direction of said sheet.
6. In an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured marginally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space, the improvement wherein said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising:
a sheet-like body of elastic material having at least one elliptical opening therethrough. the minor axis of such opening being aligned in said second direction and the major axis of such opening being aligned in said one direction;
a plurality of relatively inelastic tension cords embedded in said material and running in said one direc tion;
a plurality of relatively elastic tension cords embedded in said material and running in said second direction, there being a first separated pair of groups of relatively elastic tension cords which are parallel to each other and which are separated to delineate a space defining said major axis, there being a second separated pair of groups of relatively elastic tension cords on opposite sides of one group of said first pair, said second pair of groups criss-crossing each other and said one group at one end of said opening so that each group of said second pair is routed in a generally elongated S-shape, there being a third separated pair of groups of relatively elastic tension cords disposed on opposite sides of the other group of said first pair, said third pair of groups criss-crossing each other and said other group at the other end of said opening so that each group of said third pair is routed in a generally elongated Sshape, whereby when said trunk is un' inflated said opening is elliptical whereas when the trunk is inflated said opening assumes a generally circular shape.
7. In an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured marginally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space, the improvement wherein said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising:
a sheet-like body of elastic material having at least one elliptical opening therethrough, the minor axis of such opening being aligned in said second direction and the major axis of such opening being aligned in said one direction;
a plurality of relatively inelastic tension cords embedded in said material and running in said one direction;
a plurality of relatively elastic tension cords embedded in said material and running in said second di' rection, those elastic tension cords on one side of said opening and which otherwise would intersect therewith being divided into two first groups one of which is routed past one end of said opening is an elongated S pattern and the other of which is routed past the other end of said opening in an elongated 8 pattern, and those elastic tension cords on the other side of said opening and which otherwise would intersect therewith being divided into two further groups one of which further groups is routed past said one end of the opening in an elongated S pattern and the other of which further groups is routed past said other end of the opening in an elongated S pattern, whereby said one first group criss-crosses said one further group at said one end of the opening whereas said other first group criss-crosses said other further group at said other end of the opening so said opening is elliptical when said trunk is relaxed and is of generally circular shape when said trunk is inflated.
8. In an air cushion vehicle as defined in claim 7 wherein there are two additional groups of said relatively elastic tension cords which pass the opposite ends of said opening and are criss-crossed by the crisscrossed groups at such opposite ends of the opening.
Claims (8)
1. IN AN AIR CUSHION VEHICLE HAVING A BODY PRESENTING A BOTTOM SURFACE, AN INFLATABLE TRUNK SECURED MARGINALLY THEREOF TO SAID BOTTOM SURFACE NORMALLY TO LIE IN CONTIGUOUS RELATION THERETO, AND MEANS ASSOCIATED WITH SAID VEHICLE FOR INFLATING SAID TRUNK CAUSING IT TO BULGE AWAY FROM SAID BOTTOM SURFACE AND CIRCUMSCRIBE AN AIR CUSHION SPACE, THE IMPROEMENT WHEREIIN SAID TRUCK COMPRISES A SHEET OF MATERIAL WHICH IS RELATIVELY INELASTIC IN ONE DIRECTION AND IS RELATIVELY ELASTIC IN A SECOND DIRECTION ESSENTIALLY TRANSVERSE TO SAID ONE DIRECTION, SAID SHEET COMPRISING: A FIRST SERIES OF TAPES ASSOCIATED WITH SAID SHEET AND DISPOSED IN SIDE-BY-SIDE RELATION AND RUNNING IN SAID ONE DIRECTION, EACH TAPE OF SAID FIRST SERIES INCLUDING A MATRIX AND A PLURALITY OF RELATIVELY INELASTIC TENSION CORDS EMBEDDED IN AND RUNNING LENGTHWISE OF SUCH TAPES, AT LEAST ONE PAIR OF ADJACENT TAPES OF SAID FIRST SERIES HAVING THEIR ADJACENT SIDE EDGES SEPARATED FOR A DISTANCE IN SAID ONE DIRECTION BY A FIRST SPACING IN SAID SECOND DIRECTION, A SECOND SERIES OF TAPES ASSOCIATED WITH SAID SHEET AND RUNNING IN SAID SECOND DIRECTION WITH SAID SHEET AND SERIES INCLUDING A MATRIX AND A PLURALITY OF RELATIVELY ELASTIC TENSION CORDS EMBEDDED IN AND RUNNING LENGTHWISE OF SUCH TAPES, THERE BEING A FIRST SEPARATED PAIR OF SAID TAPES OF THE SECOND SERIES WHICH ARE PARALLEL AND ARE SEPARATED BY A SECOND SPACING WHICH IS GREATER THAN SAID FIRST SPACING WHEREBY SAID FIRST SPACE DEFINES THE MINOR AXIS OF A ELLIPSE AND SAID SECOND SPACING DEFINES THE MAJOR AXIS OF SUCH ELLIPSE, SAID ADJACENT PAIR OF TAPES OF THE FIRST SERIES BEING SEPARATED IN SAID ONE DIRECTION BY AT LEAST SAID SECOND SPACING AND SAID SEPARATED PAIR OF SAID TAPES OF THE SECOND SERIES CROSSING SAID ADJACENT PAIR SUCH THAT SAID SHEET HAS AN ELLIPTICAL OPENING THERETHROUGH DELINEATED BY SAID MINOR AND MAJOR AXES, THERE BEING A SECOND PAIR OF TAPES OF SAID SECOND SERIES DISPOSED ON OPPOSITE SIDES OF ONE OF SAID TAPES OF THE FIRST SEPARATED PAIR, SAID SECOND PAIR OF TAPES CRISS-CROSSING EACH OTHER AND SAID ONE TAPE OF THE FIRST SEPARATED PAIR AT ONE END OF SAID OPENING, THERE BEING A THIRD PAIR OF TAPES OF SAID SECOND SERIES DISPOSED ON OPPOSITE SIDES OF THE OTHER OF SAID TAPES OF THE FIRST SEPARATED PAIR, SAID THIRD PAIR OF TAPES CRISS-CROSSING EACH OTHER AND SAID OTHER TAPE OF THE FIRST SEPARATED PAIR AT THE OTHER END OF SAID OPENING WHEREBY WHEN SAID TRUNK IS UNINFLATED SAID OPENING IS ELLIPTICAL WHEREAS WHEN SAID TRUCK IS INFLATED SAID OPENING WILL ASSUME A GENERALLY CIRCULAR SHAPE.
2. In an air cushion vehicle as defined in claim 1 wherein said second pair of tapes lie on opposite sides of and in side-by-side relation to said one tape of the first pair except at the crossing region with each other and said one tape, and wherein said third pair of tapes lie on opposite sides of and in side-by-side relation to said other tape of the first pair except at the crossing region with each other and said other tape.
3. In an air cushion vehicle a sheet material fabrication as set forth in claim 1, wherein said tension cords are crowded within portions of the fabrication peripherally of said opening means to reinforce the latter.
4. In an air cushion vehicle a sheet material fabrication as set forth in claim 1, wherein all of said tension cords bypass said fabrication opening means and extend thoughout the geometric extent of said fabric sheet without interruption.
5. In an air cushion vehicle a sheet material fabrication as set forth in claim 1, wherein said opening means comprise(s) a plurality of elliptically shaped openings arranged with their major axes aligned in row form extending transversely of the relatively elastic direction of said sheet.
6. In an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured marginally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space, the improvement wherein said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising: a sheet-like body of elastic material having at least one elliptical opening therethrough, the minor axis of such opening being aligned in said second direction and the major axis of such opening being aligned in said one direction; a plurality of relatively inelastic tension cords embedded in said material and running in said one direction; a plurality of relatively elastic tension cords embedded in said material and running in said second direction, there being a first separated pair of groups of relatively elastic tension cords which are parallel to each other and which are separated to delineate a space defining said major axis, there being a second separated pair of groups of relatively elastic tension cords on opposite sides of one group of said first pair, said second pair of groups criss-crossing each other and said one group at one end of said opening so that each group of said second pair is routed in a generally elongated S-shape, there being a third separated pair of groups of relatively elastic tension cords disposed on opposite sides of the other group of said first pair, said third pair of groups criss-crossing each other and said other group at the other end of said opening so that each group of said third pair is routed in a generally elongated S-shape, whereby when said trunk is uninflated said opening is elliptical whereas when the trunk is inflated said opening assumes a generally circular shape.
7. In an air cushion vehicle having a body presenting a bottom surface, an inflatable trunk secured marGinally thereof to said bottom surface normally to lie in contiguous relation thereto, and means associated with said vehicle for inflating said trunk causing it to bulge away from said bottom surface and circumscribe an air cushion space, the improvement wherein said trunk comprises a sheet of material which is relatively inelastic in one direction and is relatively elastic in a second direction essentially transverse to said one direction, said sheet comprising: a sheet-like body of elastic material having at least one elliptical opening therethrough, the minor axis of such opening being aligned in said second direction and the major axis of such opening being aligned in said one direction; a plurality of relatively inelastic tension cords embedded in said material and running in said one direction; a plurality of relatively elastic tension cords embedded in said material and running in said second direction, those elastic tension cords on one side of said opening and which otherwise would intersect therewith being divided into two first groups one of which is routed past one end of said opening is an elongated S pattern and the other of which is routed past the other end of said opening in an elongated S pattern, and those elastic tension cords on the other side of said opening and which otherwise would intersect therewith being divided into two further groups one of which further groups is routed past said one end of the opening in an elongated S pattern and the other of which further groups is routed past said other end of the opening in an elongated S pattern, whereby said one first group criss-crosses said one further group at said one end of the opening whereas said other first group criss-crosses said other further group at said other end of the opening so said opening is elliptical when said trunk is relaxed and is of generally circular shape when said trunk is inflated.
8. In an air cushion vehicle as defined in claim 7 wherein there are two additional groups of said relatively elastic tension cords which pass the opposite ends of said opening and are criss-crossed by the criss-crossed groups at such opposite ends of the opening.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US421335A US3901988A (en) | 1973-12-03 | 1973-12-03 | Inflatable trunk for air cushion supported vehicles |
| GB46939/74A GB1491887A (en) | 1973-12-03 | 1974-10-30 | Air cushion supported vehicles |
| AU74958/74A AU483680B2 (en) | 1973-12-03 | 1974-11-01 | Inflatable trunk for air cushion supported vehicles |
| CA213,204A CA1015009A (en) | 1973-12-03 | 1974-11-07 | Inflatable trunk for air cushion supported vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US421335A US3901988A (en) | 1973-12-03 | 1973-12-03 | Inflatable trunk for air cushion supported vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3901988A true US3901988A (en) | 1975-08-26 |
Family
ID=23670085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US421335A Expired - Lifetime US3901988A (en) | 1973-12-03 | 1973-12-03 | Inflatable trunk for air cushion supported vehicles |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3901988A (en) |
| CA (1) | CA1015009A (en) |
| GB (1) | GB1491887A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4236593A (en) * | 1976-07-22 | 1980-12-02 | British Hovercraft Corporation | Air cushion vehicle flexible skirts |
| US4248320A (en) * | 1977-10-05 | 1981-02-03 | British Hovercraft Corporation Limited | Air cushion vehicle flexible skirts |
| US4279322A (en) * | 1978-04-24 | 1981-07-21 | British Hovercraft Corporation Limited | Air cushion vehicle flexible skirt assemblies |
| US4312690A (en) * | 1977-10-05 | 1982-01-26 | British Hovercraft Corporation | Method of making air cushion vehicle flexible skirts |
| US5259574A (en) * | 1990-07-06 | 1993-11-09 | Louis Carrot | Safety device for helicopters and similar equipment with rotors |
| US8118255B1 (en) * | 2008-10-03 | 2012-02-21 | Lockheed Martin Corporation | Vehicle energy absorption |
| US20130000539A1 (en) * | 2010-03-22 | 2013-01-03 | Israel Aerospace Industries Ltd. | Improved landing system |
| US11292447B2 (en) | 2019-02-28 | 2022-04-05 | Airbus Operations Limited | Configuration of landing gear assemblies for an aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2659957A (en) * | 1949-09-12 | 1953-11-24 | Julius E Lilienfeld | Weight supporting fabric |
| US3455100A (en) * | 1967-09-26 | 1969-07-15 | Goodrich Co B F | Reinforcement for elastomeric articles |
| US3485695A (en) * | 1968-01-26 | 1969-12-23 | Johnson & Johnson | Method of making a bonded poriferous non-woven textile fabric |
| US3642565A (en) * | 1968-03-21 | 1972-02-15 | Kanegafuchi Spinning Co Ltd | Composite filaments having an elastic crimping property |
| US3690401A (en) * | 1970-09-25 | 1972-09-12 | Textron Inc | Air cushion support space defining structure and stocksheet fabrication therefor |
| US3738597A (en) * | 1971-01-04 | 1973-06-12 | Textron Inc | Aircraft undercarriage |
-
1973
- 1973-12-03 US US421335A patent/US3901988A/en not_active Expired - Lifetime
-
1974
- 1974-10-30 GB GB46939/74A patent/GB1491887A/en not_active Expired
- 1974-11-07 CA CA213,204A patent/CA1015009A/en not_active Expired
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2659957A (en) * | 1949-09-12 | 1953-11-24 | Julius E Lilienfeld | Weight supporting fabric |
| US3455100A (en) * | 1967-09-26 | 1969-07-15 | Goodrich Co B F | Reinforcement for elastomeric articles |
| US3485695A (en) * | 1968-01-26 | 1969-12-23 | Johnson & Johnson | Method of making a bonded poriferous non-woven textile fabric |
| US3642565A (en) * | 1968-03-21 | 1972-02-15 | Kanegafuchi Spinning Co Ltd | Composite filaments having an elastic crimping property |
| US3690401A (en) * | 1970-09-25 | 1972-09-12 | Textron Inc | Air cushion support space defining structure and stocksheet fabrication therefor |
| US3738597A (en) * | 1971-01-04 | 1973-06-12 | Textron Inc | Aircraft undercarriage |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4236593A (en) * | 1976-07-22 | 1980-12-02 | British Hovercraft Corporation | Air cushion vehicle flexible skirts |
| US4337106A (en) * | 1976-10-31 | 1982-06-29 | British Hovercraft Corporation Ltd. | Method of making air cushion vehicle flexible skirts |
| US4248320A (en) * | 1977-10-05 | 1981-02-03 | British Hovercraft Corporation Limited | Air cushion vehicle flexible skirts |
| US4312690A (en) * | 1977-10-05 | 1982-01-26 | British Hovercraft Corporation | Method of making air cushion vehicle flexible skirts |
| US4279322A (en) * | 1978-04-24 | 1981-07-21 | British Hovercraft Corporation Limited | Air cushion vehicle flexible skirt assemblies |
| US5259574A (en) * | 1990-07-06 | 1993-11-09 | Louis Carrot | Safety device for helicopters and similar equipment with rotors |
| US8118255B1 (en) * | 2008-10-03 | 2012-02-21 | Lockheed Martin Corporation | Vehicle energy absorption |
| US20130000539A1 (en) * | 2010-03-22 | 2013-01-03 | Israel Aerospace Industries Ltd. | Improved landing system |
| US11292447B2 (en) | 2019-02-28 | 2022-04-05 | Airbus Operations Limited | Configuration of landing gear assemblies for an aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| AU7495874A (en) | 1976-05-06 |
| CA1015009A (en) | 1977-08-02 |
| GB1491887A (en) | 1977-11-16 |
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